Damping modelling
- Viscous damping, Ev = c · Δx
- Hysteretic or structural damping
- Coulomb friction (dry friction contact)
4. Viscous
C = viscous damping coeff. ξ = damping factor.
Estimation methods: peak of frequency response function (freq. domain approach); from free response (time response approach).
i = 1.
ti, ti+1 → x1, x2.
ti+1 = ti + Td = ti + 2π/ωd.
x(ti) = x1 = C · e-ξωnticos(ωdti - φ).
x(ti+1) = x2 = C · e-ξωnti+1cos(ωdti+1 - φ).
x1/x2 = e2πξ/N=LN=x.
ln x1/x2 = δ = 2πξ/√(1 - ξ2).
ξ = δ/√2π2 + δ2.
if ξ << 1 → δ = 2πξ → ξ = δ/2π.
Damping modelling
- Viscous
- Hysteretic or structural damping
- Coulomb friction (dry friction contact)
- Viscous
C: viscous damping coeff.
ξ: damping factor.
Estimation methods: peak of frequency response function (freq. domain approach); from free response (time response approach).
t₁, t₂ → x₁, x₂.
t₂ = t₁ + Td - t₁ = 2π / ωd.
x(t₁) / x(t₂) = x₁ / x₂ = C · eσt₁.
ln x₁ / x₂ = δ = -2πξ / √(1-ξ²).
ξ = δ / √(2π² + δ²).
if ξ << 1 → δ ≈ 2πξ → ξ ≈ δ / 2π.
Damping modelling
- Viscous: Fv = c. Δẋ
- Hysteretic or structural damping
- Coulomb friction (dry friction contact)
(1) Viscous
c: viscous damping coeff.
Ϛ: damping factor.
Estimation methods: peak of frequency response function (freq. domain approach); from free response (time response approach).
μ = 1.
t₁, t₂ → x₁, x₂.
t₂ = t₁ + T₀ → t₁ + 2πω.
x(t₁)/x(t₂) = x₁/x₂ = C₁.e-Ϛωₙt₁cos(ωdt₁ - φ) / C₁.e-Ϛωₙt₂cos(ωdt₂ - φ).
x₁/x₂ = e2πϚ/N=Ϛ.
ln x₁/x₂ = δ = 2πϚ / √(1-Ϛ2).
Logarithmic decrement.
Ϛ = δ/√(2π)2 + δ2.
if Ϛ << 1 → δ = 2πϚ → Ϛ = δ/2π.
For more accurate estimates, more than 2 peaks: x1, x2, ..., xi+2.
S = 1/i ln x1/xi+2.
More accurate.
We are averaging the response constant on longer part of the response essentially as we did to do when we considered 2 consecutive peaks.
2) Hysteretic damping
(Structural).
Dissipation for each cycle.
Wh = ∫ fh dx = ∫ cẋ2 dx =.
Solution under harmonic motion.
Viscous damping.
Energy dissipated by viscous damper at each loading cycle.
Hysteretic dampers.
Wh = αx02~> Experimental.
Equivalence in terms of dissipated energy:
Wv = Wh => Ceq = α/ωx0 = k/ω.
(The slope of the curve depends on k).
Structural dampers depend on ω.
c) Study the steady state response for harmonic excitation
mẍ + Ceqẋ + kx = f(t) = F0eiωt.
mẍ + h/ωiωx + kx = F0eiωt.
mẍ + (K + iωh)x = F0eiωt.
Kc = K(1+iM).
Complex stiffness; η = h/K loss factor.
x(t) = F0/K eiωt.
The reectance freq. resp. function.
H(ω) = x0/F0/k = 1/1+iM - ω2/ωn2i = 1 - ω2/ωn2 - iM.
|H(ω)| = 1/√((1 - ω2/ωn2)2 + M2).
ψ = arctan ( M/1- ω2/ωn2).
|H|1ω/ωnψ.
G(0,1) graph is not valid in this case for small frequencies because there is no more for small freq. the meaning of G for static response.
- if ω → 0 |H(ω)|= 1/√(1+M2) < 1
if ψ = arctan M ≠ 0.
- ω = ωn
|H|max = 1/M.
eq. with viscous |H|max = 1/2ζeq.
if ζ ≡ M/2.
for underdamped system → 1/√(1-c) < √2 0 < c < √2.
- Hysteretic damping is only valid in steady-state oscillatory motion
- Not suitable for initial vib...
Energy loss per cycle is independent of speed (ẋ) and.
3. Coulomb friction
Friction force: Ff = µN = µmg.
Fd = Ff sign (ẋ) = µN sign (ẋ).
EOM.
mẍ + kx ± Fd sign (ẋ) = 0.
Not linear (system goes back and forth) but we can write a linear EOM:
mẍ + kx = -Fd, ẋ ≥ 0.
mẍ + kx = Fd, ẋ < 0.
Study the free response from i.c. x(0) = xo, ẋ(0) = 0.
Motion starts if: |kxo| > 1 / µmg.
- ẍ + ωn2x = ωn2 Ff/k, x < 0
- ẍ + ωn2x = -ωn2 Ff/k, ẋ > 0
Which eq.?
If xo > 0, mass begins to move to the left ẋ < 0 ⟹ eq. 1.
x(t) = Ff/k + a cos (ωnt) + b sin (ωnt).
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